View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 66592U 26145.58682692 +.00000000 +00000-0 +55567-3 0 00006
2 66592 43.0020 342.1395 0001603 269.5299 90.5369 15.27597221 01
| Epoch (UTC): | 25 May 2026 14:05:01 |
| Eccentricity: | 0.0001603 |
| inclination: | 43.0020° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 342.1395° |
| argument of perigee: | 269.5299° |
| revolutions per day: | 15.27597221 |
| mean anomaly at epoch: | 90.5369° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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